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Ensinger PEI

Aluminum 2025-T6
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 2000 Series Aluminum Alloy

Material Notes: Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
Composition information provided by the Aluminum Association and is not for design.

Key Words: UNS A92025; Aluminium 2025-T6; AA2025-T6; Al2025-T6
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Physical PropertiesMetricEnglishComments
Density 2.81 g/cc0.102 lb/in³AA; Typical
 
Mechanical PropertiesMetricEnglishComments
Hardness, Brinell 110110AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 138138Converted from Brinell Hardness Value
Hardness, Rockwell A 44.244.2Converted from Brinell Hardness Value
Hardness, Rockwell B 6969Converted from Brinell Hardness Value
Hardness, Vickers 124124Converted from Brinell Hardness Value
Tensile Strength, Ultimate 400 MPa58000 psiAA; Typical
Tensile Strength, Yield 255 MPa37000 psiAA; Typical
Elongation at Break 19 %
@Diameter 12.7 mm
19 %
@Diameter 0.500 in
AA; Typical
Modulus of Elasticity 71.7 GPa10400 ksiAA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Poissons Ratio 0.330.33Estimated from trends in similar Al alloys.
Fatigue Strength 124 MPa
@# of Cycles 5.00e+8
18000 psi
@# of Cycles 5.00e+8
completely reversed stress; RR Moore machine/specimen
Shear Modulus 27.0 GPa3920 ksiEstimated from similar Al alloys.
Shear Strength 241 MPa35000 psiAA; Typical
 
Electrical PropertiesMetricEnglishComments
Electrical Resistivity 0.00000432 ohm-cm
@Temperature 20.0 °C
0.00000432 ohm-cm
@Temperature 68.0 °F
AA; Typical
 
Thermal PropertiesMetricEnglishComments
CTE, linear  22.7 µm/m-°C
@Temperature 20.0 - 100 °C
12.6 µin/in-°F
@Temperature 68.0 - 212 °F
AA; Typical; average over range
 24.5 µm/m-°C
@Temperature 20.0 - 300 °C
13.6 µin/in-°F
@Temperature 68.0 - 572 °F
Specific Heat Capacity 0.880 J/g-°C0.210 BTU/lb-°FEstimated from trends in similar Al alloys.
Thermal Conductivity 154 W/m-K1070 BTU-in/hr-ft²-°FAA; Typical at 77°F
Melting Point 521 - 640.6 °C970 - 1185 °FAA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
Solidus 521 °C970 °FAA; Typical
Liquidus 640.6 °C1185 °FAA; Typical
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 90.9 - 95.2 %90.9 - 95.2 %As remainder
Chromium, Cr <= 0.10 %<= 0.10 %
Copper, Cu 3.9 - 5.0 %3.9 - 5.0 %
Iron, Fe <= 1.0 %<= 1.0 %
Magnesium, Mg <= 0.05 %<= 0.05 %
Manganese, Mn 0.40 - 1.2 %0.40 - 1.2 %
Other, each <= 0.05 %<= 0.05 %
Other, total <= 0.15 %<= 0.15 %
Silicon, Si 0.50 - 1.2 %0.50 - 1.2 %
Titanium, Ti <= 0.15 %<= 0.15 %
Zinc, Zn <= 0.25 %<= 0.25 %

References for this datasheet.

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